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A Longitudinal Control Feel System For In Flight Research On Response Feel


A Longitudinal Control Feel System For In Flight Research On Response Feel
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A Longitudinal Control Feel System For In Flight Research On Response Feel


A Longitudinal Control Feel System For In Flight Research On Response Feel
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Author : Stanley Faber
language : en
Publisher:
Release Date : 1961

A Longitudinal Control Feel System For In Flight Research On Response Feel written by Stanley Faber and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with categories.


An adjustable feel system connected to the longitudinal control system of a transonic fighter airplane has been developed and has been evaluated in flight. Variable control feel including response feel is provided from the following five sources: control position, control rate, normal acceleration, pitching velocity, and pitching acceleration. This system provides a very flexible tool for more detailed study of longitudinal control feel characteristics than has previously been possible. The evaluation program for the variable-feel system yielded flight time histories which illustrate effects on the stability of airplane and control-system response modes of large amounts of response feel. These results illustrate the need for balancing the amounts of feel from normal acceleration and pitching acceleration to maintain the stability of the short-period and control-system modes. At the frequency of the short-period mode, large amounts of normal-acceleration feel cause the control system to oscillate and excite the airplane short-period mode of oscillation. At the same frequency the pitching acceleration component of feel, which leads the normal-acceleration component by 180 deg, is almost equivalent to viscous damping on the stick. However, at slightly frequencies the lag of the response-feel components increases by 90 deg or more so that a large pitching-acceleration component excites an oscillation of the control system at 4 cycles per second. These results by confirming and supplementing the conclusions of previous observers indicate that the adjustable feel system is operating properly.



Effects Of Control Feel Configuration On Airplane Longitudinal Control Response


Effects Of Control Feel Configuration On Airplane Longitudinal Control Response
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Author : Harold L. Crane
language : en
Publisher:
Release Date : 1961

Effects Of Control Feel Configuration On Airplane Longitudinal Control Response written by Harold L. Crane and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with Aerodynamic load categories.




Nasa Technical Note


Nasa Technical Note
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Author :
language : en
Publisher:
Release Date : 1961

Nasa Technical Note written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with categories.




Human Engineering


Human Engineering
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Author : Defense Documentation Center (U.S.)
language : en
Publisher:
Release Date : 1962

Human Engineering written by Defense Documentation Center (U.S.) and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1962 with Human engineering categories.




Index To Nasa Technical Publications


Index To Nasa Technical Publications
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Author : United States. National Aeronautics and Space Administration
language : en
Publisher:
Release Date : 1960-07

Index To Nasa Technical Publications written by United States. National Aeronautics and Space Administration and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1960-07 with categories.




A Selected Listing Of Nasa Scientific And Technical Reports For


A Selected Listing Of Nasa Scientific And Technical Reports For
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Author :
language : en
Publisher:
Release Date : 1960

A Selected Listing Of Nasa Scientific And Technical Reports For written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1960 with Aeronautics categories.




Index Of N A S A Technical Publications


Index Of N A S A Technical Publications
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Author : United States. National Aeronautics and Space Administration
language : en
Publisher:
Release Date : 1960

Index Of N A S A Technical Publications written by United States. National Aeronautics and Space Administration and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1960 with categories.




Monthly Catalog Of United States Government Publications


Monthly Catalog Of United States Government Publications
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Author :
language : en
Publisher:
Release Date : 1961

Monthly Catalog Of United States Government Publications written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with Government publications categories.




Analysis Of Longitudinal Pilot Induced Oscillation Tendencies Of Yf 12 Aircraft


Analysis Of Longitudinal Pilot Induced Oscillation Tendencies Of Yf 12 Aircraft
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Author : Flight Research Center (U.S.)
language : en
Publisher:
Release Date : 1975

Analysis Of Longitudinal Pilot Induced Oscillation Tendencies Of Yf 12 Aircraft written by Flight Research Center (U.S.) and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1975 with Airplanes categories.




Proceedings


Proceedings
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Author :
language : en
Publisher:
Release Date :

Proceedings written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on with Airplanes categories.